Mathematical Model of a Satellite with an Arbitrary Number of Flexible Appendages
| العنوان: | Mathematical Model of a Satellite with an Arbitrary Number of Flexible Appendages |
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| المؤلفون: | A. I. Shestopyorov, Stepan Sergeevich Tkachev, M. Yu. Ovchinnikov |
| المصدر: | Mathematical Models and Computer Simulations. 13:638-647 |
| بيانات النشر: | Pleiades Publishing Ltd, 2021. |
| سنة النشر: | 2021 |
| مصطلحات موضوعية: | Cantilever, Spacecraft, Computer science, business.industry, Dynamics (mechanics), Hinge, Equations of motion, Topology, Computational Mathematics, Generalized coordinates, Modeling and Simulation, Rewriting, Articulation (phonetics), business |
| الوصف: | A mathematical model of a spacecraft (SC) with an arbitrary number of large flexible structural (appendages) elements (LFSEs) is developed, implemented, and verified. The SC model obtained based on the general equations of dynamics is written in generalized coordinates. It allows three types of articulation between the LFSEs and the SC’s body: cantilever, and with the help of one-step and two-step hinges. Due to the procedure used in the derivation of the equations of motion, the proposed model allows us to change the number of LFSEs and types of articulation without rewriting the equations of motion in symbolic form, which makes it comfortable for software implementation. |
| تدمد: | 2070-0490 2070-0482 |
| DOI: | 10.1134/s2070048221040190 |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=doi_________::0c8b44c9b0b94e827185c4634ef7a708 https://doi.org/10.1134/s2070048221040190 |
| Rights: | CLOSED |
| رقم الانضمام: | edsair.doi...........0c8b44c9b0b94e827185c4634ef7a708 |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 20700490 20700482 |
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| DOI: | 10.1134/s2070048221040190 |